N802US, cancelled Feb 6, 2006

Service difficulty reports · 33

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N802US' AND deregistration_id = 'N802US-2006-02-06'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR USAAD01161Light · inoperativeBOS - THE AFT RIGHT EXIT WINDOW EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M)Sep 19, 2001 · N802US · Doug DC981 · Emergency LightingSDR USAAD01142Door · not closedTPA-PIT - FLT 302 - AFTER TAKEOFF AND THE LANDING GEAR WAS RETRACTED, THERE WAS A LOUD VIBRATION FROM THE NOSE WHEEL DOORS. THE LANDING GEAR WAS CYCLED WITH THE SAME RESULTS. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND Jul 31, 2001 · N802US · Doug DC981 · Landing Gear Door Retract SectionSDR USAAD01136Battery · dischargedBOS - THE AFT LOW LEVEL EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M)Jul 11, 2001 · N802US · Doug DC981 · Emergency LightingSDR USAAD01087Battery · dischargedIND - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)Apr 30, 2001 · N802US · Doug DC981 · Emergency LightingSDR USAAD01036Power Supply · inoperativeEWR - FOUND SEVERAL CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED THE POWER SUPPLY AT SEAT 25. (M)Feb 20, 2001 · N802US · Doug DC981 · Emergency LightingSDR USAAD01031Light · misinstalledMCO - A CONFIGURATION DEVIATION WAS FOUND IN THE OVERHEAD EMERGENCY LIGHTS SYSTEM. THE LIGHT BULB IN THE RIGHT EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 31 WAS REMOVED, LEAVING THE UNIT BLAND, TO COMPLY WITH THE CORRECT CONFIGURATION. (M)Feb 16, 2001 · N802US · Doug DC981 · Emergency LightingSDR USAAD00151Bottle · dischargedBDL - THE AFT LEFT SERVICE DOOR EVACUATION SLIDE INFLATION BOTTLE HAD LOW PRESSURE. MAINTENANCE REPLACED THE AFT LEFT SERVICE DOOR EVACUATION SLIDE. (M)Sep 24, 2000 · N802US · Doug DC981 · Escape SlideSDR USAAD00129Strut · dischargedPIT-BNA - FLT 961 - AFTER TAKEOFF, THE NOSE LANDING GEAR DID NOT RETRACT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED THE NOSE LANDING GEAR STRUT. (M)Aug 13, 2000 · N802US · Doug DC981 · Nose/Tail Landing Gear Strut/AxleSDR USAA001043Finger Doubler · corrodedPIT - Q-5 - FINGER DOUBLERS, 2 INCHES LONG BY 2 INCHES WIDE, CORROSION; LEVEL 1; TASK NR C51-53300. SKIN LAP FINGER DOUBLER STA 576 - STA 588 UNDER LONGERON 26L. CUT OUT DAMAGED PART AND SPLICED IN NEW SECTION PER SRM 53-04 FIG 50. (X)Jul 18, 2000 · N802US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA001045Beltframe · crackedPIT - Q-5 - BELTFRAME, .50 INCH CRACK, STA 1322 LONGERON 17R. CUT OUT DAMAGED SECTION AND SPLICED IN NEW PER SRM 53-03, PAGE 129. (X)Jul 18, 2000 · N802US · Doug DC981 · Fuselage Main, FrameSDR USAA001044Seat Track · damagedPIT - Q-5, SEAT TRACK, 1 INCH BY .50 INCH AREA, CORROSION LEVEL 1, TASK NR C46-53303, STA 229 LEFT OUTBOARD SEAT TRACK. CUT SEAT TRACK, REMOVED DAMAGED SECTION, AND SPLICED IN NEW STA 200 - STA 250 PER SRM 53-05 FIG 4F. (X)Jul 18, 2000 · N802US · Doug DC981 · Fuselage, Seat/Cargo Attach FittingsSDR USAA000974Web · corrodedPIT - FOUND CUSP MEMBRANE CORRODED 2 INCHES BY 2 INCHES, AFT SVC DOOR LOWER JAMB STATION 1165. INSTALLED DOUBLER PER EA 55543. (M)Jun 30, 2000 · N802US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAAD00040Light · failedTPA - THE LEFT AFT SERVICE DOOR AND THE RIGHT AFT EXIT WINDOW EMERGENCY LIGHTS WERE NOT OPERATING PROPERLY. MAINTENANCE REPLACED THE LEFT AFT SERVICE DOOR AND RIGHT AFT EXIT WINDOW EMERGENCY LIGHTS. (M)Mar 13, 2000 · N802US · Doug DC981 · Emergency LightingSDR USAAD99186Escape Slide · failedPIT - DURING ANNUAL OPERATIONAL CHECK OF THE AFT SERVICE DOOR ESCAPE SLIDE, THE ESCAPE SLIDE DID NOT INITIALLY INFLATE AS THE ESCAPE SLIDE HUNG ON GIRT BAR SEVERAL MINUTES UNTIL BEING JIGGLED, THEN INFLATED. ALSO, THE ESCAPE SLIDE MOUNTED EMERGENCY LIGHTS FAIDec 24, 1999 · N802US · Doug DC981 · Escape SlideSDR USAAD99189Battery · dischargedCLT - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED 8 AISLE LIGHT BATTERIES, 1 CONTROL MODULE BATTERY, AND 1 AFT SERVICE DOOR LIGHT ASSEMBLY. (M)Dec 15, 1999 · N802US · Doug DC981 · Emergency LightingSDR 2000ZZZM224Light · failedCLT - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED 8 AISLE LIGHT BATTERIES, 1 CONTROL MODULE BATTERY, AND 1 AFT SERVICE DOOR LIGHT ASSEMBLY. (M)Dec 15, 1999 · N802US · Doug DC981 · Emergency LightingSDR 2000ZZZM223Battery · dischargedCLT - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED 8 AISLE LIGHT BATTERIES, 1 CONTROL MODULE BATTERY, AND 1 AFT SERVICE DOOR LIGHT ASSEMBLY. (M)Dec 15, 1999 · N802US · Doug DC981 · Emergency LightingSDR USAAD99153Battery · dischargedCLT - THE FORWARD OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD OVERWING EMERGENCY LIGHT BATTERIES. (M)Oct 26, 1999 · N802US · Doug DC981 · Emergency LightingSDR USAAD99072Battery · dischargedPIT - PILOT REPORTED THE LOW LEVEL EMERGENCY LIGHTING WAS INOPERATIVE DURING ORIGINATING PREFLIGHT CHECK. MAINTENANCE REMOVED AND REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES. OPERATIONAL CHECK GOOD. (M)Jun 3, 1999 · N802US · Doug DC981 · Emergency LightingSDR USAAD99064Fuel Control · failedPIT-DFW - FLT 1588 - DURING CRUISE, THE CREW ATTEMPTED TO ADJUST THE LEFT ENGINE THRUST SETTING BUT THERE WAS NO RESPONSE TO THE THROTTLE LEVER MOVEMENT. THE ENGINE POWER STAYED ON 90 PERCENT N1. DURING APPROACH FOR LANDING AT THE DESTINATION THE LEFT ENGINEMay 13, 1999 · N802US · Doug DC981 · Fuel Control/Turbine EnginesSDR USAAD98153Rt Pack · failedCLT-IND - FLT 1128 - AFTER TAKEOFF, THE LEFT AIR CONDITIONING PACK QUIT OPERATING AND THE AIRCRAFT WOULD NOT PRESSURIZE. THE RIGHT AIR CONDITIONING PACK WAS ON MEL. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE RAN THE LEFT AIRAug 29, 1998 · N802US · Doug DC981 · Cabin Cooling SystemSDR USAAD97003Engine · failedFLT 1020 - RSW-CLT - DURING CLIMB, A LOUD BAND WAS HEARD, AND THE NR 2 ENGINE EPR WENT TO 1.0. CREW REDUCED ENGINE TO IDLE, AND DIVERTED TO MCO. ENGINE WAS SHUT DOWN AFTER LANDING. REPLACED ENGINE. (M)Jan 5, 1997 · N802US · Doug DC981 · Engine (Turbine/Turboprop)SDR USAAD96174Power Supply · failedFORWARD AND MID CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN MID CABIN POWER SUPPLY. REPLACED POWER SUPPLY AND BATTERIES IN FORWARD CABIN. (M)Nov 27, 1996 · N802US · Doug DC981 · Emergency LightingSDR USAAD96148Batteries · dischargedFLOOR TRACK LIGHTING ROWS 3-10 INOP. REPLACED BATTERIES IN FORWARD POWER PACK. (M)Oct 16, 1996 · N802US · Doug DC981 · Emergency LightingSDR USAAD96050Battery Pack · dischargedFLT 7003 - ROC - CEILING MOUNTED EMERGENCY LIGHTS BETWEEN ROWS 5 AND 7 INOP. FOUND DURING OVERNIGHT CHECK. REPLACED BATTERIES IN POWER PACK. OPERATIONAL CHECK OK. (M)May 8, 1996 · N802US · Doug DC981 · Emergency LightingSDR USAA960203Frame · corrodedPIT - DURING Q-4 INSPECTION, FOUND CORROSION 3 FEET BY 2 INCHES WIDE ON PREVIOUS REPAIR DOUBLER BETWEEN STATION 1154 - STATION 1211 AFT CARGO DOOR LOWER FRAME. CORROSION LEVEL 1 TASK NR C57-53300. MANUALLY INSTALLED REPAIR DOUBLERS PER USAIR EO NR 5390M251. Feb 2, 1996 · N802US · Doug DC981 · Fuselage Main, FrameSDR USAA960202Longeron · corrodedPIT - DURING Q-4 INSPECTION, FOUND LEVEL 1 CORROSION AT LONGERON 29L STATION 1231-1250 AROUND AND AT RIVETS. CORROSION TASK NR C57-53300. SPLICED IN NEW SECTION OF LONGERON PER USAIR EA 31905. (M)Feb 2, 1996 · N802US · Doug DC981 · Fuselage Main, Longeron/StringerSDR USAA960201Longeron · corrodedPIT - DURING Q-4 INSPECTION, FOUND LEVEL 1 CORROSION ON LONGERON 30 FROM STATION 1285 TO STATION 1295. CORROSION TASK NR C57-53300. CUT OUT CORRODED SECTION OF LONGERON AND ACCOMPLISHED SPLICE REPAIR PER DACO DWG 5936667. (M)Feb 2, 1996 · N802US · Doug DC981 · Fuselage Main, Longeron/StringerSDR USAA960200Skin · crackedPIT - DURING Q-4 INSPECTION, FOUND 1 INCH CRACK AT STATION 1437 LONGERON 3R IN FUSELAGE SKIN. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 27. (M)Feb 2, 1996 · N802US · Doug DC981 · Fuselage Main, Plate/SkinSDR USAA950773Slide · malfunctionedDCA - WHILE INSPECTING THE TAIL AREA FOR FUEL FUMES, THE TAILCONE WAS INADVERTENTLY DEPLOYED. THE TAIL SLIDE DID NOT DEPLOY. THE SLIDE WAS RERIGGED WITH THE TAIL CONE LANYARD TO DETERMINE THE REASON FOR THE SLIDE NOT DEPLOYING. MAINTENANCE RERIGGED THE SLIDJul 21, 1995 · N802US · Doug DC981 · Emergency EquipmentSDR USAA950430Door Pan · corrodedIND - DURING CD-2 INSPECTION, FOUND CORROSION ON AFT SIDE OF FORWARD DOOR STOP FITTING IN LOWER SILL PAN. CUT OUT CORRODED AREA AND INSTALLED SPLICE REPAIR PER SRM 53-05 FIG 44 AND USAIR EA 29986. (M)Mar 19, 1995 · N802US · Doug DC981 · Fuselage Miscellaneous StructureSDR USAA950254Angle · crackedIND - DURING SCHEDULED CX-2 INSPECTION, FOUND A 1 INCH CRACK EXTENDING FROM VERTICAL LEG INTO HORIZONTAL LEG OF STABILIZER TO FUSELAGE ATTACH ANGLE. CUT OUT DAMAGED SECTION AND INSTALLED FILLER AND REPAIR DOUBLER PER SRM 53-05 FIG NR 23A. (W)Mar 17, 1995 · N802US · Doug DC981 · Fuselage, Stabilizer Attach FittingsSDR USAA950107Oil Line · inoperativeCLT - FLT 1133 - THE LEFT ENGINE OIL QUANTITY DROPPED TO ZERO, AND THE OIL PRESSURE ALSO DROPPED. THE ENGINE WAS SHUTDOWN AND FLIGHT DIVERTED TO CLT. MAINTENANCE REPLACED THE OIL LINE TO THE OIL PRESSURE SWITCH AND THE FILTERS. OPERATIONS CHECKED GOOD. (Z)Feb 8, 1995 · N802US · Doug DC981 · Engine Oil Distribution (Airframe Furnished)
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